View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 10011U 26072.96305245 +.00000000 +00000-0 -11239-3 0 00007
2 10011 65.8625 276.8433 0692259 73.2721 38.5118 12.32266597 04
| Epoch (UTC): | 13 March 2026 23:06:47 |
| Eccentricity: | 0.0692259 |
| inclination: | 65.8625° |
| perigee height: | 991 km |
| apogee height: | 2088 km |
| right ascension of ascending node: | 276.8433° |
| argument of perigee: | 73.2721° |
| revolutions per day: | 12.32266597 |
| mean anomaly at epoch: | 38.5118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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